In this paper, separation control on Joukowsky airfoil having leading edge rotational cylinder is investigated by numerical simulation method.
本文使用数值模拟方法研究了活动翼面对翼型背风面分离的控制作用。
In this paper, separation control on Joukowsky airfoil having leading edge rotational cylinder is investigated by numerical simulation method.
本文使用数值模拟方法研究了活动翼面对翼型背风面分离的控制作用。
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